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NPFC - MIL-HDBK-221

Fire Protection Design Handbook for U.S. Navy Aircraft Powered by Turbine Engines

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Organization: NPFC
Publication Date: 22 April 2014
Status: active
Page Count: 1

Document History

MIL-HDBK-221
April 22, 2014
Fire Protection Design Handbook for U.S. Navy Aircraft Powered by Turbine Engines
A description is not available for this item.
MIL-HDBK-221
December 27, 1995
FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
This Handbook embodies requirements and design objectives for fire protection for all types of manned Naval aircraft (including helicopters) with turbine engines.
MIL-HDBK-221
May 3, 1965
FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
This Handbook embodies requirements and design objectives for fire protection for all types of manned Naval aircraft (including helicopters) with turbine engines.

References

This document references:
API RP 2003 - Protection Against Ignitions Arising Out of Static, Lightning, and Stray Currents
Published by API on September 1, 2015
General This recommended practice (RP) presents the current state of knowledge and technology in the fields of static electricity, lightning, and stray currents applicable to the prevention of...
This document is referenced by:
MIL-HDBK-516 - AIRWORTHINESS CERTIFICATION CRITERIA
Published by NPFC on December 12, 2014
This document establishes the airworthiness certification criteria, standards and methods of compliance to be used in the determination of airworthiness of all manned and unmanned, fixed and rotary...
This document is referenced by:
DEF STAN 00-970: PART 0 - Certification Specifications for Airworthiness Part 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Published by MODUK on March 14, 2021
Part 0 provides guidance and content information, together with definitions of terms used throughout this Standard.
This document is referenced by:
DEF STAN 00-970: PART 5 - Certification Specifications for Airworthiness Part 5: LARGE TYPE AIR SYSTEMS
Published by MODUK on March 14, 2021
Where CS 25 makes reference to ‘the Agency’, this should be considered to mean the certifying authority.
This document is referenced by:
DEF STAN 00-970: PT7 SEC1 - Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Section 1: Introduction
Published by MODUK on July 13, 2015
This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Rotorcraft Aircraft for UK Military operation.
This document is referenced by:
DEF STAN 00-970: PT1 SEC4 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 4: Design and Construction
Published by MODUK on July 13, 2015
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
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